High stiffness shape memory alloy actuated aerostructure
A shape memory alloy (SMA) actuated aerostructure operable to dynamically change shape according to flight conditions is disclosed. Deformable structures are actuated by SMA actuators that are coupled to face sheets of the deformable structures. Actuating the SMA actuators produces complex shape changes of the deformable structures by activating shape changes of the SMA actuators. The SMA actuators are actuated via an active or passive temperature change based on operating conditions. The SMA actuated aerostructure can be used for morphable nozzles such as a variable area fan nozzle and/or a variable geometry chevron of a jet engine to reduce engine noise during takeoff without degrading fuel burn during cruise.
1. A shape memory alloy actuated aerostructure comprising:
a first face sheet;
a second face sheet; and
at least one shape memory alloy actuator comprising one layer of shape memory alloy metal coupled to the first face sheet at at least one first location on the first face sheet and coupled to the second face sheet at a plurality of second locations on the second face sheet and operable to obtain an optimum area for a variable area fan nozzle by morphing the shape memory alloy actuated aerostructure thereby reducing noise, the at least one first location and the second locations located at substantially maxima and minima of the at least one shape memory alloy actuator respectively.
2. The shape memory alloy actuated aerostructure of claim 1 , wherein the at least one shape memory alloy actuator is operable to deform the shape memory alloy actuated aerostructure in at least two dimensions.
3. The shape memory alloy actuated aerostructure of claim 1 , wherein a shape of the at least one shape memory alloy actuator comprises at least one of the group consisting of: essentially sinusoidal, a lattice, an I-beam, strips, and connected strips.
4. The shape memory alloy actuated aerostructure of claim 1 , wherein the shape memory alloy actuated aerostructure comprises at least one of the group consisting of: a variable area fan nozzle panel, and a variable geometry chevron.
5. The shape memory alloy actuated aerostructure of claim 1 , wherein the shape memory alloy actuated aerostructure is coupled to at least one of the group consisting of: a fan nozzle, and a core nozzle.
6. The shape memory alloy actuated aerostructure of claim 1 , wherein the shape memory alloy actuated aerostructure is coupled to at least one part of a thrust reverser sleeve.
7. The shape memory alloy actuated aerostructure of claim 1 , wherein the at least one shape memory alloy actuator is passively controlled by temperature.
8. The shape memory alloy actuated aerostructure of claim 1 , wherein the at least one shape memory alloy actuator is coupled to the first face sheet and the second face sheet by a method comprising at least on one of the group consisting of: adhering, brazing, welding, fastening, and bonding.
9. The shape memory alloy actuated aerostructure of claim 1 , wherein a shape of the at least one shape memory alloy actuator comprises a lattice.
10. The shape memory alloy actuated aerostructure of claim 1 , wherein a shape of the at least one shape memory alloy actuator comprises an I-beam.
11. The shape memory alloy actuated aerostructure of claim 1 , wherein:
the at least one shape memory alloy actuator comprises a sinusoidal strip of shape memory alloy metal; and
the at least one first location and the second locations are located at substantially maxima and minima of the sinusoidal strip respectively.
12. A system for morphing an aerostructure, the system comprising:
at least one shape memory alloy actuated aerostructure comprising:
a first face sheet;
a second face sheet; and
at least one shape memory alloy actuator comprising one layer of shape memory alloy metal coupled to the first face sheet at at least one location on the first face sheet and coupled to the second face sheet at a plurality of locations on the second face sheet and operable to obtain an optimum area for a variable area fan nozzle by morphing the shape memory alloy actuated aerostructure thereby reducing noise, the first location and the second locations located at substantially maxima and minima of the at least one shape memory alloy actuator respectively; and
a controller operable to activate at least one region of the at least one shape memory alloy actuator to morph the at least one shape memory alloy actuated aerostructure.
13. The system of claim 12 , wherein the at least one shape memory alloy actuated aerostructure extends from a lip area of the nozzle in proximity to a flow path of a gas flow emitted from the nozzle.
14. The system of claim 13 , wherein the at least one shape memory alloy actuated aerostructure is deformable between a first position in proximity to the flow path to a second position extending into the flow path.
15. The system of claim 13 , wherein the at least one shape memory alloy actuated aerostructure is deformable from a first position in proximity to the flow path to a second position extending away from the flow path.
16. The system of claim 13 , further comprising shaping the at least one shape memory alloy actuator in response to a temperature change to obtain an optimum area for the nozzle by morphing the shape memory alloy actuated aerostructure based on at least one flight condition.
17. The system of claim 12 , wherein a shape of the at least one shape memory alloy actuator comprises a lattice.
18. The system of claim 12 , wherein a shape of the at least one shape memory alloy actuator comprises an I-beam.
19. The system of claim 12 , wherein:
the at least one shape memory alloy actuator comprises a sinusoidal strip of shape memory alloy metal; and
the at least one first location and the second locations are located at substantially maxima and minima of the sinusoidal strip respectively.